EGYPTSAT A, 44047
Orbit data source: Space-Track
EGYPTSAT A, 44047 is a payload satellite owned by EgSA (EG) in SSO that was launched on Thu, 21 Feb 2019 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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44047 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / EGYPRelated business
Manufacturer
Yuzhnoe
Mission
Operational Civil Imaging
Bus & Motor
EGYPTSAT, Unknown motor
Mass
~1,050 kg wet, ~1,050 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan + 1 Ant, 1.0 m
Radar Cross Section
0.867 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 EGYPTSAT A
1 44047U 19008A 25259.32756572 .00000614 00000-0 10475-3 0 9998
2 44047 98.0110 323.1323 0001245 108.9443 251.1900 14.72372819352943Epoch: 2025-09-16T07:51Z
TLE epoch observation values (Epoch: 2025-09-16T07:51:41.678Z)
Latitude
0.00005°
Longitude
-150.31082°
Altitude
656.793 km
Speed
7.529 km/s
True Right ascension
21h 32m 31s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:58:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
651.434 km
Perigee altitude
649.684 km
Semi-major axis
7,028.696 km
Eccentricity
0.00012
Inclination
98.011°
RAAN
323.1323°
Arg. of periapsis
108.9443°
True anomaly
251.1765°
Mean anomaly
251.19°
Eccentric anomaly
251.18325°
Mean motion
3.68325 °/min
Orbital period
97.74 mins
BSTAR
0.00010475
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Other satellites on launch #8 in the year 2019 (2019-02-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.EGYPTSAT A Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-16 16:35:15.527Z | 32.4° NE | 2025-09-16 16:39:15.527Z | 96.932° ESE | 28.899° | 2025-09-16 16:43:15.527Z | 161.963° S |
| 4 mins | 2025-09-16 18:14:15.527Z | 321.639° NNW | 2025-09-16 18:16:15.527Z | 284.377° WNW | 20.359° | 2025-09-16 18:18:15.527Z | 252.512° W |
| 6 mins | 2025-09-17 03:35:15.527Z | 115.492° SE | 2025-09-17 03:37:15.527Z | 79.321° E | 25.272° | 2025-09-17 03:41:15.527Z | 11.845° NNE |
| 5 mins | 2025-09-17 05:12:15.527Z | 224.58° SW | 2025-09-17 05:14:15.527Z | 261.582° W | 23.103° | 2025-09-17 05:17:15.527Z | 313.215° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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